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Contents

   



(Top)
 


1 Development  





2 Design  





3 Operational history  





4 Variants  





5 Operators  



5.1  Current  





5.2  Former  







6 Similar weapons  





7 Photo Gallery  





8 Notes  





9 References  














Kh-15






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From Wikipedia, the free encyclopedia
 

(Redirected from Raduga Kh-15)

Raduga Kh-15
(NATO reporting name: AS-16 'Kickback')
Raduga Kh-15
TypeAir-launched ballistic missile
Air-to-ground missile
Anti-radiation missile (Kh-15P)
Anti-ship missile (Kh-15S)
Place of originSoviet Union
Service history
In service1980
Used byRussia
Production history
DesignerRaduga
Designed1974–1980
ManufacturerDubna Machine-building Plant
Produced1980
Specifications
Mass1,200 kg (2,650 lb)
Length478 cm (15 ft 8 in)
Diameter45.5 cm (17.9 in)
Wingspan92 cm (36.2 in) maximum
Warheadconventionalornuclear
Warhead weight150 kg (331 lb)
Blast yield300 kt

Enginesolid-fuel RDTT-160

Operational
range

300 km (160 nmi)
Flight ceiling40,000 m (130,000 ft)
Maximum speed Up to Mach 5[1]

Guidance
system

inertial guidance, active radar homing, or anti-radiation missile

Launch
platform

Tu-22M3, [1]

The Raduga Kh-15orRKV-15 (Russian: Х-15; NATO: AS-16 "Kickback"; GRAU:) is a Russian hypersonic aero-ballistic air-to-ground missile carried by the Tupolev Tu-22M and other bombers. Originally developed as a standoff nuclear air-to-ground missile similar to the U.S. Air Force's AGM-69 SRAM, versions with conventional warheads have been developed.

As of early 2019, it was uncertain whether the Kh-15 was in service, with rumors that it had been retired or placed in storage.[2]

Development

[edit]

In 1967, MKB Raduga started developing the Kh-2000 as a replacement for the Kh-22 (NATO reporting name AS-4 Kitchen) heavy anti-shipping missile.[1] Development of the Kh-15 started some time in the early 1970s.[3] The sophistication of the design made it suitable for other roles, and a nuclear-tipped version was developed in tandem with the conventionally armed variant.[1] An upgrade under development was cancelled in 1991, but reports in 1998 suggested an upgraded Kh-15 might be fitted to Su-35 (Flanker-E) tactical aircraft.[3]

Design

[edit]

The Kh-15 climbs to an altitude of about 40,000 m (130,000 ft) and then dives in on the target, accelerating to a speed of about Mach 5.[1]

Operational history

[edit]

It entered service in 1980. It can be carried by the Su-33, Su-34, Tu-95MS-6 'Bear-H', Tu-22M3 'Backfire C', and Tu-160 'Blackjack'.[4]

Variants

[edit]

Operators

[edit]

Current

[edit]

Former

[edit]

Similar weapons

[edit]
[edit]

Notes

[edit]
  1. ^ a b c d e f "Kh-15, RKV-15 (AS-16 'Kickback')", Jane's Air-Launched Weapons, 2008-08-01, archived from the original on 2019-10-18, retrieved 2009-02-03
  • ^ Kristensen, Hans M.; Korda, Matt (4 March 2019). "Russian nuclear forces, 2019". Bulletin of the Atomic Scientists. 75 (2): 73–84. Bibcode:2019BuAtS..75b..73K. doi:10.1080/00963402.2019.1580891.
  • ^ a b "Kh-15 (AS-16 'Kickback'/RKV-15)", Jane's Strategic Weapon Systems, 2008-09-02, archived from the original on 2019-10-18, retrieved 2009-02-06
  • ^ "АО "Корпорация Тактическое Ракетное Вооружение"". Archived from the original on 2014-08-06. Retrieved 2016-08-25.
  • References

    [edit]
    Retrieved from "https://en.wikipedia.org/w/index.php?title=Kh-15&oldid=1221422000"

    Categories: 
    Anti-radiation missiles of the Soviet Union
    Cold War air-to-surface missiles of the Soviet Union
    Cold War anti-ship missiles of the Soviet Union
    Air-launched ballistic missiles
    Air-to-surface missiles of the Soviet Union
    Anti-ship missiles of the Soviet Union
    MKB Raduga products
    Nuclear air-to-surface missiles
    Military equipment introduced in the 1980s
    Hidden categories: 
    Articles with short description
    Short description is different from Wikidata
    Articles containing Russian-language text
     



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